GB2132367B - Thrust and airflow monitor for aeroengine test cells - Google Patents

Thrust and airflow monitor for aeroengine test cells

Info

Publication number
GB2132367B
GB2132367B GB08232151A GB8232151A GB2132367B GB 2132367 B GB2132367 B GB 2132367B GB 08232151 A GB08232151 A GB 08232151A GB 8232151 A GB8232151 A GB 8232151A GB 2132367 B GB2132367 B GB 2132367B
Authority
GB
United Kingdom
Prior art keywords
thrust
test cells
airflow monitor
aeroengine test
aeroengine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB08232151A
Other versions
GB2132367A (en
Inventor
Philip Andrew Simpson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB08232151A priority Critical patent/GB2132367B/en
Priority to US06/541,314 priority patent/US4537066A/en
Priority to FR8317465A priority patent/FR2535847B1/en
Priority to DE19833340516 priority patent/DE3340516A1/en
Priority to JP58211676A priority patent/JPS59182331A/en
Publication of GB2132367A publication Critical patent/GB2132367A/en
Application granted granted Critical
Publication of GB2132367B publication Critical patent/GB2132367B/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/13—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the tractive or propulsive power of vehicles
    • G01L5/133—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the tractive or propulsive power of vehicles for measuring thrust of propulsive devices, e.g. of propellers
GB08232151A 1982-11-10 1982-11-10 Thrust and airflow monitor for aeroengine test cells Expired GB2132367B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB08232151A GB2132367B (en) 1982-11-10 1982-11-10 Thrust and airflow monitor for aeroengine test cells
US06/541,314 US4537066A (en) 1982-11-10 1983-10-12 Aeroengine test cells
FR8317465A FR2535847B1 (en) 1982-11-10 1983-11-03 AIRCRAFT ENGINE TEST CELLS
DE19833340516 DE3340516A1 (en) 1982-11-10 1983-11-09 METHOD AND SYSTEM FOR CORRECTING NET SHEET MEASUREMENTS IN AN AIRCRAFT ENGINE TEST CELL
JP58211676A JPS59182331A (en) 1982-11-10 1983-11-10 Test cell for aircraft engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08232151A GB2132367B (en) 1982-11-10 1982-11-10 Thrust and airflow monitor for aeroengine test cells

Publications (2)

Publication Number Publication Date
GB2132367A GB2132367A (en) 1984-07-04
GB2132367B true GB2132367B (en) 1986-01-15

Family

ID=10534176

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08232151A Expired GB2132367B (en) 1982-11-10 1982-11-10 Thrust and airflow monitor for aeroengine test cells

Country Status (5)

Country Link
US (1) US4537066A (en)
JP (1) JPS59182331A (en)
DE (1) DE3340516A1 (en)
FR (1) FR2535847B1 (en)
GB (1) GB2132367B (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5293775A (en) * 1992-11-02 1994-03-15 United Technologies Corporation Gas turbine engine test cell
US5831155A (en) * 1996-12-02 1998-11-03 Atlantic Research Corporation Apparatus and method for simulating rocket-to-ramjet transition in a propulsion system
GB2384058B (en) 2002-01-15 2005-11-30 Rolls Royce Plc Thrust correction
JP4339016B2 (en) * 2002-05-20 2009-10-07 川崎重工業株式会社 Thrust distribution method and thrust distribution apparatus
GB2438431B (en) * 2006-05-25 2008-08-20 Rolls Royce Plc Thrust correction
DE102008041916B3 (en) * 2008-09-09 2010-01-21 Anecom Aerotest Gmbh Test device for fan i.e. engine blower, of aircraft engine for determination of e.g. performance data, has measuring devices and microphone connected to modularly formed telemetry unit and exchangeably arranged in bypass flow channel
DE102011013517B4 (en) 2011-03-10 2012-10-11 Airbus Operations Gmbh Propeller system with two contra-rotating propellers, method for detecting the thrust of a propeller system with two contra-rotating propellers and wind tunnel with a propeller system arranged therein model
CN106092420B (en) * 2016-05-26 2017-05-17 中国人民解放军63820部队吸气式高超声速技术研究中心 Method for indirectly measuring effective thrust of engine
US10364698B2 (en) * 2016-06-10 2019-07-30 Rolls-Royce North American Technologies, Inc. System and method of non-intrusive thrust measurement
FR3070761B1 (en) * 2017-09-07 2019-08-23 Safran Aircraft Engines METHOD AND DEVICE FOR MEASURING A PUSH MARGIN OF A TURBOMACHINE
CN108197342B (en) * 2017-11-28 2021-12-28 中国航发沈阳发动机研究所 Method for calculating non-design air leakage of air system of aircraft engine
CN110779679B (en) * 2019-11-21 2021-01-26 中国空气动力研究与发展中心低速空气动力研究所 Method for correcting influence of pressure compensation chamber of calibration box on high-precision force measuring balance
CN112129484A (en) * 2020-10-12 2020-12-25 中铁西南科学研究院有限公司 Method for testing head pressure loss coefficient of high-speed train dynamic model test
CN114001964B (en) * 2021-11-02 2024-02-02 中国航发沈阳发动机研究所 Flight table with large-span S-bend air inlet and exhaust system
CN116296418B (en) * 2022-08-18 2024-01-16 中国航空工业集团公司北京长城计量测试技术研究所 Large-space flow field characteristic parameter testing method based on distributed cross section

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA998770A (en) * 1971-10-29 1976-10-19 John R.B. Murphy Method and apparatus for determining the thrust of a jet engine
CA1160345A (en) * 1972-08-31 1984-01-10 George B. Mackintosh Determination of gross thrust-related parameters
US4034604A (en) * 1975-09-29 1977-07-12 The Boeing Company Apparatus for determining characteristics of turbo-powered airplane engine simulators

Also Published As

Publication number Publication date
GB2132367A (en) 1984-07-04
FR2535847B1 (en) 1986-12-19
JPS59182331A (en) 1984-10-17
FR2535847A1 (en) 1984-05-11
US4537066A (en) 1985-08-27
DE3340516A1 (en) 1984-05-10

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19931110